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FORCED LANDING DETECTION SYSTEM AND METHOD FOR DETECTION OF AN AIRCRAFT FORCED LANDING

机译:迫降检测系统和飞机迫降检测方法

摘要

forced landing detection system, and method for detecting a forced landing of an aircraft. a hard landing detection system includes a wheel assembly, a shock absorber mechanically coupled to the wheel assembly and landing gear assembly landing gear, a controller that has a processor, and configured non-transient tangible memory to communicate with the processor. tangible, non-transient memory has instructions stored in it, which, in response to processor execution, cause the hard landing detection system to perform operations including the detection of a landing event through the processor and the determination through the processor if the landing event is hard. The hard landing system may further include the use of the stroke position sensor and landing event detection may include the use of the stroke position sensor to measure a stroke profile of the shock absorber. Additionally, determining whether the landing event is hard may include purchasing, through the processor, the impact damper stroke profile for a predetermined maximum impact damper stroke.
机译:强制降落检测系统以及用于检测飞机的强制降落的方法。硬着陆检测系统包括:轮组件;与轮组件和起落架组件起落架机械耦合的减震器;具有处理器的控制器,以及配置为与处理器通信的非瞬态有形存储器。有形的非瞬态存储器中存储有指令,这些指令响应于处理器的执行,使硬着陆检测系统执行操作,包括通过处理器检测着陆事件以及通过处理器确定着陆事件是否为硬。硬着陆系统可以进一步包括使用行程位置传感器,并且着陆事件检测可以包括使用行程位置传感器来测量减震器的行程轮廓。另外,确定着陆事件是否很困难可以包括通过处理器为预定的最大冲击阻尼器冲程购买冲击阻尼器冲程轮廓。

著录项

  • 公开/公告号BR102017027196A2

    专利类型

  • 公开/公告日2019-02-19

    原文格式PDF

  • 申请/专利权人 GOODRICH CORPORATION;

    申请/专利号BR20171027196

  • 发明设计人 ADNAN CEPIC;AMIR FAZELI;SUSANNE REBER;

    申请日2017-12-15

  • 分类号B64C25;B64C25/28;B64C25/60;B64D45;

  • 国家 BR

  • 入库时间 2022-08-21 12:03:41

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